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737 Electronic Test Equipment

(ALPHA-NUMERIC BY MAIN P/N)

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Main P/N C34001


End Item -1


Aero Info P/N 34-B37-1309


Title Adapter Assy LSI FMC/COU, ATS. Used to provide test capability for the Lear-Siegler FMC/CDU on the ATS-182.


Notes Applicable to 737-300,-400,-500 after line #2566 with a 10-62225 FMC installed.
Applicability
Supersedes
Replaces


737-300
737-400
737-500


Main P/N C34004


End Item -1


Aero Info P/N 34-B37-1572


Title Circuit Board Assy - Detector, ARINC 429 - Label FF. Used to provide test capability for the Smiths (LSI) FMC/CDU on the ATS-182.


Notes
Applicability
Supersedes
Replaces


737-500


Main P/N C34005


End Item -1


Aero Info P/N



Title Extended Box - Radio Altimeter Receiver Transmitter. Used in place of Radio Altimeter (RA) Receiver - Transmitter (RT) primarily AlliedSignal Model ALA-52B RA RT.


Notes
Applicability
Supersedes
Replaces


737-600
737-700
737-800
737-900


Main P/N C34006


End Item -57


Aero Info P/N 34-MUL-1607


Title Adapter, Tray - EFIS Symbol Generator Software Loading. Used to load software into the S242T404 EFIS symbol generator.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500

C34006-53
C34006-53
C34006-53
Main P/N C34011


End Item -11


Aero Info P/N 34-B37-1573


Title Adapter Assy - Honeywell MCP/FCC ATS. Used to provide test capability for the Honeywell MCP/FCC on the ATS-182.


Notes
Applicability
Supersedes
Replaces


737-300
737-400


Main P/N C34011


End Item -12


Aero Info P/N 34-B37-1573


Title Adapter Assy - Honeywell MCP/FCC ATS. Used to provide test capability for the Honeywell MCP/FCC on the ATS-182.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500


Main P/N C34012


End Item -2


Aero Info P/N 34-B37-1511


Title Test Box - Total Air Temperature Probe, Air Data System. Used during test of the Air Data System to connect decade resistance box in place to total air temperature probe per Maintenance Manual Chapter 34-12-00.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-ADV
737-CQC

Main P/N C34012


End Item -21


Aero Info P/N 34-B37-1511


Title Test Box - Total Air Temperature Probe, Air Data System. Used during test of the Air Data System to connect decade resistance box in place to total air temperature probe per Maintenance Manual Chapter 34-12-00.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-ADV
737-CQC
C34012-1
C34012-1
C34012-1
C34012-1
C34012-1
C34012-1
C34012-1
C34012-1
C34012-1
C34012-1

Main P/N C49002


End Item -1


Aero Info P/N 49-B37-1574


Title Test Box - APU Control Unit. Used to perform LRU (Line Replaceable Unit) functional test and SRU (Shop Repairable Unit) troubleshooting for the APU Control Unit.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500


Main P/N C71012


End Item -35


Aero Info P/N 71-B37-1310


Title Test Equipment - Engine Vibration Isolation. Used to verify the source of engine vibration.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500


Main P/N C71012


End Item -47


Aero Info P/N 71-B37-1310


Title Test Equipment - Engine Vibration Isolation. Used to verify the source of engine vibration.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500

C71012-28
C71012-28
C71012-28
Main P/N C72001


End Item -1


Aero Info P/N 72-B37-1575


Title Indicator Overlay Set - Airborne Vibration
Monitoring. Used to improve readability of the Airborne Vibration Monitoring System Indicator during engine trim operations.



Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500


Main P/N C73002


End Item -1


Aero Info P/N



Title Test Box - P5-68 Power Management Control Module. Used to bench test the P5-68 Module.


Notes
Applicability
Supersedes
Replaces


737-600
737-700
737-800


Main P/N C75001


End Item -1


Aero Info P/N 75-B37-1576


Title Switch, Patent - System Test. Used to hold the Air-Gnd-Nose sensing pushbutton switches in the depressed position during functional testing.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500


Main P/N C77001


End Item -31


Aero Info P/N 77-B37-1311


Title Test Box - Engine Accessory Unit. Used to test Engine Accessory Unit assembly.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500
C77001-14, -18, -28
C77001-14, -18, -28
C77001-14, -18, -28

Main P/N C77002


End Item -20


Aero Info P/N 77-B37-1252


Title Test Box - Tachometer System. Used to simulate N1 & N2 tachometer output during engine tachometer system test, Autothrottle System test, & Stall Warning System tests per Maintenance Manuals.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500
C77002-1
C77002-1
C77002-1

Main P/N C77003


End Item -1


Aero Info P/N 77-B37-1312


Title Test Box - P.C. Cards, Engine Accessory Unit. Used to test Engine Accessory Unit printed circuit assemblies.




Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500


Main P/N C77004


End Item -10


Aero Info P/N 77-MUL-1512


Title Test Box - Generic AVM Interface. Used to provide user interface between ARINC 429 transmitter/receiver (customer furnished) and the generic airborne vibration monitor, for acquiring fault and flight history.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500
737-600
737-700
737-800
737-900
C77004-1
C77004-1
C77004-1
C77004-1
C77004-1
C77004-1
C77004-1

Main P/N F70303


End Item -1


Aero Info P/N 31-MUL-1226


Title Tachometer - Engine Trim, Remote. Connects to the N2 Tachometer System Test Receptacle in the control cabin. This places remote tach in parallel with selected eng tach ind to check accuracy.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC


Main P/N F70303


End Item -2


Aero Info P/N 31-MUL-1226


Title Tachometer - Engine Trim, Remote. Connects to the N2 Tachometer System Test Receptacle in the control cabin. This places remote tach in parallel with selected eng tach ind to check accuracy.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC


Main P/N F70303


End Item -3


Aero Info P/N 31-MUL-1226


Title Tachometer - Engine Trim, Remote. Connects to the N2 Tachometer System Test Receptacle in the control cabin. This places remote tach in parallel with selected eng tach ind to check accuracy.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC


Main P/N F70316


End Item -140


Aero Info P/N 28-MUL-1338


Title Auxiliary Defueling External Power Control Unit.Used to defuel an aircraft using an external ground power source.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-ADV
737-CQC

F70316-1
F70316-1
F70316-1
F70316-1
F70316-1
Main P/N F70328


End Item -1


Aero Info P/N 70-MUL-1601


Title Probe - Film Resistance Measuring. Used with multimeter to measure resistance of electrical bond between conductive coating on non-conductive plastic sheet and the grounding fasteners.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-ADV
737-CQC


Main P/N F72731


End Item -81


Aero Info P/N



Title Adapter Assy & Fuel & Oil Qty Test Sets. Used to isolate faulty fuel & oil quantity indicating system components. Note: See current drawing for dash number applicability.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC


Main P/N F72731


End Item -82


Aero Info P/N



Title Adapter Assy & Fuel & Oil Qty Test Sets. Used to isolate faulty fuel & oil quantity indicating system components. Note: See current drawing for dash number applicability.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC


Main P/N F72785


End Item -573


Aero Info P/N 24-MUL-1187


Title Test Set - Elevator, Rudder, Aileron PCU. Used to test the elevator, rudder and aileron power control units. See drawing for additional test cables required.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC

F72785-551
F72785-551
F72785-551
F72785-551
Main P/N F72891


End Item -1


Aero Info P/N 49-MUL-1290


Title Indicator - APU RPM, Test Set. Provides a means of observing the APU speed during troubleshooting situations at Auxiliary Power Unit locations.


Notes Used on APU's without an electronic speed switch.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC


Main P/N F72891


End Item -20


Aero Info P/N 49-MUL-1290


Title Indicator - APU RPM, Test Set. Provides a means of observing the APU speed during troubleshooting situations at Auxiliary Power Unit locations.


Notes Used on APU's without an electronic speed switch.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC


Main P/N F72917


End Item -19


Aero Info P/N 29-MUL-1255


Title Test Equipment - Ground Fault Protection System, Hydraulic System B., Abex Pumps. To provide for functional testing of the hydraulic system B pump motor ground fault protection system.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500
737-600
737-700
737-800
F72917-1
F72917-1
F72917-1
F72917-1
F72917-1
F72917-1

Main P/N F72989


End Item -1


Aero Info P/N 34-MUL-1258


Title Cable - Directional Gyro Extension. Used to connect the Sperry Directional Gyro (2588302-4) to A/P wiring when mounted on the tilt/rotational table for directional reference system testing.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC


Main P/N F72998


End Item -15


Aero Info P/N 77-MUL-1294


Title Adapter Cable - N1 Simulator. Used to connect tachometer tester in place of the N1 tach transmitters to simulate N1 signals for testing full flight regime autothrottle systems.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC

F72998-1
F72998-1
F72998-1
F72998-1
Main P/N F73015


End Item -20


Aero Info P/N 31-MUL-1259


Title Test Box - Stall Warning Module. Used to test the Stall Warning Module per OHM 31-15-01 and 31-15-02.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
F73015-1
F73015-1

Main P/N F80129


End Item -100


Aero Info P/N 32-B37-1208


Title Antiskid - Auto Brake - Auto Speed Brake Tester. Used to check out the skid control and auto brake system.


Notes Used on airplanes with Hydro-Aire Anti-Skid System. Goodyear Anti-Skid System use F80208.
Applicability
Supersedes
Replaces


737-ADV
737-CQC


Main P/N F80135


End Item -1


Aero Info P/N 29-MUL-1296


Title Cable Assembly - Hydraulic Leakage Check. To determine hydraulic leakage by measuring the current draw of the electric motor driven hydraulic pump.


Notes Used on 737 System "B" electric pumps. The -10 is used on 737 Standby Hydraulic Pumps.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-ADV
737-CQC


Main P/N F80135


End Item -10


Aero Info P/N 29-MUL-1296


Title Cable Assembly - Hydraulic Leakage Check. To determine hydraulic leakage by measuring the current draw of the electric motor driven hydraulic pump.


Notes Used on 737 System "B" electric pumps. The -10 is used on 737 Standby Hydraulic Pumps.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-600
737-700
737-800
737-ADV
737-CQC


Main P/N F80138


End Item -1


Aero Info P/N 34-MUL-1251


Title Extension Cable - Vertical Gyro. Connects the Tilt Table with A/P wiring for reference system testing. For A/P equipped with Bendix vertical gyro.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC


Main P/N F80139


End Item -1


Aero Info P/N 34-MUL-1198


Title Extension Cable - Vertical Gyro. Used to connect vertical gyro on the Tilt Table with A/P wiring for attitude reference system testing, Sperry Gyro.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC


Main P/N F80165


End Item -42


Aero Info P/N 34-MUL-1198


Title Test Set - Door Proximity Sensor/Actuator Gap. Used on Door Warning System to check that actuator-to-sensor gap is correctly adjusted & to verify integrity of sensor-to-switch module wiring.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC

F80165-1
F80165-1
F80165-1
F80165-1
F80165-1
F80165-1
F80165-1
Main P/N F80206


End Item -1


Aero Info P/N N 24-B37-1262


Title Breakout Box - Cabin Pressure Control Unit. Used to check voltages from test connector on cabin pressure controller on P/N 763810-1 & -2.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC


Main P/N F80208


End Item -1


Aero Info P/N 32-B37-1499


Title Tester - Anti-skid/Autospeed Brake. Used to check wheel speed transducers with anti-skid system functional test. Simulates input signal to anti-skid control from wheel speed transducers.


Notes Used on airplanes with Goodyear Anti-Skid System. Hydro-Aire Anti-Skid System use F80129.

Applicability
Supersedes
Replaces


737-100
737-200
737-CQC

2TE6545113
2TE6545113
2TE6545113
Main P/N F80217


End Item -139


Aero Info P/N 22-B37-1265


Title Test Set, SP177/SP300 Autopilot Rudder/Elevator/Aileron. Used to operate the SP177 Autopilot System during control rigging.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500
737-ADV
737-CQC
F80217-125
F80217-125
F80217-125
F80217-125
F80217-125

Main P/N F80218


End Item -40


Aero Info P/N 27-B37-1313


Title Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC
F80218-1
F80218-1
F80218-1
F80218-1

Main P/N F80218


End Item -41


Aero Info P/N 27-B37-1313


Title Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.


Notes
Applicability
Supersedes
Replaces


737-300
737-400
737-500
737-ADV
737-CQC
F80218-31
F80218-31
F80218-31
F80218-31
F80218-31

Main P/N F80218


End Item -42


Aero Info P/N 27-B37-1313


Title Test Set - Force Transducer, Control Wheel Steering. Used to operate the CWS force transducers during control rigging.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
F80218-38
F80218-38
F80218-38
F80218-38
F80218-38
F80218-38
F80218-38

Main P/N F80221


End Item -1


Aero Info P/N 80-B37-1263


Title Test Set - Proximity Sensors T/R. Used to supply 28VDC power to the T/R upper and lower door lock prox sensors. Provides the proper proximity sensor indication during T/R operation.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC


Main P/N F80224


End Item -60


Aero Info P/N 80-B37-1605


Title Test Eqpt - Flight Spoiler Power Control Unit. Used to conduct functional test after overhaul of Flight Spoiler Power Control Units.


Notes
Applicability
Supersedes
Replaces


737-600
737-700
737-800
737-900
F80224-58
F80224-58
F80224-58
F80224-58

Main P/N F80225


End Item -19


Aero Info P/N 22-B37-1521


Title SP177 Dual Channel FCC Test Equipment. Used to check the SP177 Dual Channel Autopilot Computers.


Notes
Applicability
Supersedes
Replaces


737-ADV
737-CQC

F80225-1
F80225-1
Main P/N F80227


End Item -1


Aero Info P/N 80-B37-1577


Title Test Cable - N1 Simulation. Adapts a signal generator to aircraft test receptacle D556 to simulate N1 tach generator signal for testing full range autothrottle system.


Notes Applicable only to 737-200 aircraft with full range auto throttle speed control computer P/N 10-61985; digital electronic N1 tachometer indicator P/N 10-61991, and test receptacle D556.
Applicability
Supersedes
Replaces


737-ADV


Main P/N F80228


End Item -15


Aero Info P/N 80-B37-1578


Title Adapter Cable - N1 Simulator. Used to connect tach tester in place of the N1 tachometer transmitter to simulate N1 signals for testing full flight autothrottle system per MM.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-ADV
737-CQC

F80228-1
F80228-1
F80228-1
F80228-1
Main P/N F80229


End Item -57


Aero Info P/N 26-MUL-1297


Title Tester - Fire Extinguishing System. Used to test the electrical wiring continuity of the engine and APU fire extinguishing systems.


Notes See T&E for dash number applicability.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC

F80229-17
F80229-17
F80229-17
F80229-17
F80229-17
F80229-17
F80229-17
Main P/N F80229


End Item -58


Aero Info P/N 26-MUL-1297


Title Tester - Fire Extinguishing System. Used to test the electrical wiring continuity of the engine and APU fire extinguishing systems.


Notes See T&E for dash number applicability.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
F80229-18
F80229-18
F80229-18
F80229-18
F80229-18
F80229-18
F80229-18

Main P/N F80229


End Item -59


Aero Info P/N 26-MUL-1297


Title Tester - Fire Extinguishing System. Used to test the electrical wiring continuity of the engine and APU fire extinguishing systems.


Notes See T&E for dash number applicability.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
F80229-19
F80229-19
F80229-19
F80229-19
F80229-19
F80229-19
F80229-19

Main P/N F80229


End Item -60


Aero Info P/N 26-MUL-1297


Title Tester - Fire Extinguishing System. Used to test the electrical wiring continuity of the engine and APU fire extinguishing systems.


Notes See T&E for dash number applicability.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
F80229-21
F80229-21
F80229-21
F80229-21
F80229-21
F80229-21
F80229-21

Main P/N F80229


End Item -61


Aero Info P/N 26-MUL-1297


Title Tester - Fire Extinguishing System. Used to test the electrical wiring continuity of the engine and APU fire extinguishing systems.


Notes See T&E for dash number applicability.
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
F80229-49
F80229-49
F80229-49
F80229-49
F80229-49
F80229-49
F80229-49

Main P/N F80237


End Item -13


Aero Info P/N 31-B37-1314


Title Test Set Equipment Cooling System Performance. Used for the adjustment and test of the equipment cooling system.


Notes
Applicability
Supersedes
Replaces


737-100
737-200
737-300
737-400
737-500
737-ADV
737-CQC
F80237-1
F80237-1
F80237-1
F80237-1
F80237-1
F80237-1
F80237-1

Main P/N G23001


End Item -32


Aero Info P/N 23-MUL-1546


Title Test Box - RCP Processor Card. Used for testing and troubleshooting the Radio Communications Panel Processor.


Notes
Applicability
Supersedes
Replaces


737-300
G23001-23

Main P/N J22004


End Item -54


Aero Info P/N



Title Test Eqpt - Autothrottle Gearbox, Brake. Used in the run-in and Acceptance Test Procedures for Autothrottle Brake (254W4101), Rudder Control Brake (253W3349), and Autothrottle Gearbox Brake (254W140) Assemblies. The J22004-1, -54 are for 50 Hz Power Systems and the J22004-2, -55 are for 60 Hz.


Notes
Applicability
Supersedes
Replaces


737-600
737-700
737-800
737-900


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